M MoTIS AIRCRAFT INNOVATION ON A DAILY BASIS
HOME MoTIS PROFESSIONAL CASE STUDIES IN VIRTUAL EXPERIMENTAL TECHNOLOGY
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M MoTIS AIRCRAFT INNOVATION ON A DAILY BASIS |
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HOME MoTIS PROFESSIONAL CASE STUDIES IN VIRTUAL EXPERIMENTAL TECHNOLOGY |
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| VERT-LEV STUDY | SUPER VTOL | PTV STUDY | OGGY UNITS | MED EVAC STUDY | HOVER JET STUDY | VECTOR JET |
THE MoTIS AIR BENDER
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THE MoTIS VERT-LEV PROJECT
EXPERIMENTAL LOGISTICS STUDY 000-121-YW-VERT INTRODUCTION: A COMPLETE CASE STUDY INTO THE THEORY OF FIXED PITCH WHIRLING WING PROPS AND THERE POTENTIAL USE IN INTERSTATE MASS AERIAL TRANSPORT BY TEAM MoTIS DEVELOPMENT STAFF
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ELECTRONIC TABLE OF CONTENTS
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INTRODUCTION: A COMPLETE CASE STUDY INTO THE THEORY OF FIXED PITCH WHIRLING WING PROPS AND THERE POTENTIAL USE IN INTERSTATE MASS AERIAL TRANSPORT
BY TEAM MoTIS DEVELOPMENT STAFF
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AIRCRAFT INTRO: Welcome to the first day of posted information on what will become known to you as the VERTICAL MASS TRANSITS INTERSTATE LEVITATION SYSTEM.
The VERT-LEV system is a complete virtual study developed by team MoTIS internal staff on a super cheap and fuel efficient aerial mass transit system! We have been working on this system, using flight simulations to test out our virtual theoretical logistics systems and are now ready to share with our viewing and buying public! This whole logistical system comes almost entirely out of the mind of MoTIS CEO and founder. O WATSON is the official developer of the AIR BENDER aircraft at AIR RAIL LOGISTICS SYSTEM, along with Jennifer Guess. This is in no way a recreation of any kind and is a total and original concept logistical system being simulated into the world of Microsoft Flight Simulator platform programs. P1 |
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EXPERIMENTAL LOGISTICS STUDY 000-121-YW-VERT THE ACTUAL AIR RAIL SYSTEM So what is this VERT-LEV project all about, you may ask? Well the goal of VERT -LEV is to research, design, and develop a cost effective solution to a potential and realistic mass interstate transportations system. team MoTIS has coined this concept the MoTIS MASS TRAN AIR RAIL SYSTEM.- MO-MATARS for short.
The MoTIS development staff has already started building the virtual scenery infrastructure to support this intensive research study. The ideology is that we have already got numerous GPS satellites in orbit around the planet, and we are going to use this technology Virtually that is) to design a safe interstate ultra low altitude high way in the sky. This will become the actual AIR RAIL system itself. P2 |
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THE ACTUAL NEO CONCEPT AIRCRAFT TECHNOLOGY Team MoTIS has long had a VTOL development wing operation at our virtual XROW labs, and have just recently decided on an interesting piece of VTOL/STOL equipment to do the job with in this type of mass transportation system. Welcome the MoTIS AIR BENDER SUPER STOL UTILITY VEHICLE.
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Graphical Representations:
FULL DATA COMING SOON |
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As there are numerous was to convey information in then present age of information, we at team MoTIS are adopting a new and efficient way o f sharing our data and info with you. Only known as the E-BOOK CONCEPT, we will be totally abandoning any presentations in standard PDF format, and word document format , for what most online surfers are already use to! The HTML online style layout. THE E-BOOK CONCEPT is not a new concept in the since that it is something new, but in the since that we are creating a certain style and presents to our information layouts that will be presented to you in this complete actual online book layout format. We will present you with numerous book cover jackets, graphic binders, and more! Best of all the note book in the FS program that we develop for will allow you to open any and all of our materials right inside your cockpit so that you can read on those long flight!
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AIRCRAFT SPECS:
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Graphical Representations:
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EXPERIMENTAL LOGISTICS STUDY 000-121-YW-VERT SWIRLUX AIR TORQUE 2000
This AIR BENDER is s super unique research aircraft in the fact that is not a helicopter, and not a true VTOL aircraft, but is instead a partial whirling fixed wing lift device conceived by team MoTIS development staff. Here is a break down of where the VERT-LEVS would fall under a general current standard aircraft category of today.
This aircraft is solely designed to operate with in the AIR RAIL SYSTEM and is not classed as a general purpose aircraft at all. The VERT -LEVS are to be classified as SUPER STOL aircraft. These aircraft can best be described as rotating wings! As the aircraft have now VTOL dynamics at all. Their over all usefulness is in the fact that they can take off and land in almost nonsensically short distances! This SUPER STOL dynamics performance characteristic will allow for special VEER-LEV aircrafts to be built on top of existing buildings as totally new VERT LEV airports.
The VERT -LEV theoretical principle is simple. Use a Hugh high density whirling wing to generated the needed take off lift , and use a standard pusher thrust producing device to propel the aircraft into forward flight! The aircraft generate what is virtual suspected as a lift cylinder, which is totally controlled via a special throttle and governor built into the engine. The aircraft generates excessive vertical lift and then with the help of special stabilizers placed around the aircraft, is lifted genially into the heavens!. There are two sets of throttles in the VERT-LEVS. One controls the lifting turbine engine and the other the horizontal thrusting turbine. This type of aircraft is governed totally by the amount of lift that can be generated by engine out put values.
AIRCRAFT STABILITY CONTROLS The aircrafts lack wings and are all controlled by multiple stabilizer projects out of the sides of the fuselage.
ROLL MOMENTS
PITCH MOMENTS
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HOW THE AIR BENDER TRANSPORTER WORKS
First of all the VERT-LEVS do not exhibit any VTOL abilities what so ever. These aircraft lack full physical fixed wings and instead generate all lift for two counteracting high density high pitched whirling wing units!
THE AERODYNAMICS EQUILIBRIUM BALANCING ACT This principle works exactly like a standard propeller accept the fact that the SWIRLUX unit is massive and needs to generate very small RPMS to generate excessive lift capacities, due to the radius of the WING PROP lifting blades. the aircraft fly's exactly like a conventional fixed wing aircraft except the fact that she is SUPER STOL capable!
The AIR BENDER first achieves the right among of RPM, which give you the proper amount of actual lift generated above the aircraft, the aircraft is fully flight ready! MASSIVE PROOF OF CONCEPT COMING SOON VIA EXCEL DATA LABS
AIR BENDER TAKE OFF PERFORMANCE SPECS
The AIR BENDER will have the ability to carry mass passenger and cargo loads and to transition from ground operations and into flight very quickly. The standard rating cycle for the lift generation system needs to generate at approximately 25% above maximum allowable loaded take off weights. The aircraft is therefore designed with greater engine out put then the over all weight of the aircraft, providing power stroke torque inputs into the fixed Wing/Prop blades P5 |
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EXPERIMENTAL LOGISTICS STUDY 000-121-YW-VERT PANEL AND VISIBILITY
Sample first stage panel documentation
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VERT-LEV THEORY MATH
In theory let us say that the aircraft weights 3500lbs and the turbine is generation a turbine shaft torque of 3000 RPMS. each RPM setting has a total lift setting. So at maximum RPM the total lifting capacity of the VERT-LEVS give us a new lift rating in this particular neo concept aircraft in question, known as VLT max.
For all of our theoretical study models using X PLANE and MSFS we will rate this total lifting capacity at 25% of the total weight of our aircraft in question.
If our VERT-LEV lets say weights 3500 lbs then our VLT max lift rating will be 3500 x .25= 875 lbs lift excess on this particular aircraft.3500 + 875= 4375lbs this concept actually gives each aircraft super torque lifting capacities. P7 |
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GUTS TECHNICAL DRAWING : The first guts system to preview on this aircraft will be the AIR BENDER custom gear system, now under development by GUTS primary designer. AIRCRAFT SUB-SYSTEMS
Our resident CATIA developer is working on a great new great system design for the MoTIS AIR BENDER neo concept aircraft! This gear system will be fully developed in AUTO CAD, CATIA, and FSDS V3!
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E BOOK END COVER CREDITS AND EXTENDED SUBJECT
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ADDITIONAL ATTENTION: Please member that team MoTIS is fueled with college students and real world aerodynamics students and our mission is not simulated for the pure hobbyist only.
NOTICE: This experimental aircraft is not a helicopter, gyroplane, convertiplane, or heliplane. It is a virtual study in a theoretical whirling winged aircraft. The CO-AXIAL MOUNTED WING-PROP- AKA TWISTERS, as we are defining it, is a lift generating device that the team MoTIS development staff if working on mathematical proximity equations for. We will post this data in full at the end of the study in the form of an online case study paper in word perfect. This is an original idea and the intellectual property of team MoTIS development staff. All rights reserved.
Note: All of these concept aircraft and experimental logistics systems are from the design staff of the MoTIS CAD engineering board and our CEO. We do not copy others work or design real world concept aircraft at all. Each of our aircraft are from our heads and are the sole intellectual property of MoTIS and we can prove it. We take great pride in all of our true concept designs and do not create real world aircraft, model aircraft variants or concepts, or other designers concept work at all ,but stand by our mission statement in truly creating "OUR OWN DESIGNS"
MoTIS VIRTUAL JET DESIGN is a leading virtual FS neo concept aircraft manufacturer with the most modern and extensive product line.
